# Service difficulty reports: N601EN

A list on [N601EN](https://openairdocs.org/aircraft/N601EN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR VNAA20260125015](https://openairdocs.org/sdr/VNAA20260125015.md): Fitting · corroded · Jan 4, 2026 · N601EN · Bombdr CL6002D15 · Fuselage Main, Attach Fittings
  > CORROSION ON MACHINED FITTINGS, FROM BS 517 & 565, AND FROM BS 629 & 661+16 ON CTR DOOR IN FWD CARGO BAY. THE MACHINED FITTINGS WERE EVALUATED OUT OF LIMITS IAW SRM 53-32-58-101-001-A01 AND WERE REPLACED IAW SRM 51-42-10-001-001-A01, SRM 51-42-21-001-001-
- [SDR VNAA20260125009](https://openairdocs.org/sdr/VNAA20260125009.md): Support · corroded · Jan 4, 2026 · N601EN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACKS ON AFT DIAPHRAGM, BOTH (LBL17 & RBL17) AT AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE. THE AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE WAS REPAIRED IAW REO 690-53-82-263 REV -, AND IAW REO 690-53-82-261 REV -.
- [SDR VNAA20260125021](https://openairdocs.org/sdr/VNAA20260125021.md): Skin · dented · Jan 1, 2026 · N601EN · Bombdr CL6002D15 · Nacelle/Pylon, Plate/Skin
  > SEVERAL DENTS BTW 4 O'CLOCK TO 7 O'CLOCK EXTERNAL SKIN OF THE LOWER FAN COWL DOOR AT LT ENGINE. SEVERAL DENTS BTW 4 O'CLOCK TO 7 O'CLOCK EXTERNAL SKIN OF LOWER FAN COWL DOOR AT LT ENGINE WERE REPAIRED IAW REO 670-54-14-1012, REV B.
- [SDR VNAA20260125020](https://openairdocs.org/sdr/VNAA20260125020.md): Fitting · corroded · Dec 16, 2025 · N601EN · Bombdr CL6002D15 · Buffet/Galleys
  > CORRODED FLOOR FITTING ACCESS 107, AISLE SIDE AND BEHIND ACCESS 108 ON GALLEY 1. FLOOR FITTING ACCESS 107 AISLE SIDE AND BEHIND ACCESS 108 PN, CDSP2019-7C-760 WERE REPLACED IAW CMM 25-33-21.
- [SDR VNAA20260125019](https://openairdocs.org/sdr/VNAA20260125019.md): Fairing · worn · Dec 14, 2025 · N601EN · Bombdr CL6002D15 · Vertical Stabilizer
  > WEAR AND NICKS ON METALLIC CONTACT SURFACE OF LT VENTRAL FIN FAIRING. WEAR AND NICKS ON METALLIC CONTACT SURFACE OF LT VENTRAL FIN FAIRING WERE BLEND OUT PER REO 690-53-87-011 REV -.
- [SDR VNAA20260125018](https://openairdocs.org/sdr/VNAA20260125018.md): Hinge Fitting · worn · Dec 13, 2025 · N601EN · Bombdr CL6002D15 · Rudder Structure
  > FREE PLAY ON BEARING OF RUDDER HINGE FITTING NR 3 AT REAR SPAR OF HORIZONTAL STABILIZER. RUDDER HINGE FITTING NR 3 AT REAR SPAR OF HORIZONTAL STABILIZER WAS REPLACED IAW RIL 2103, REV B.
- [SDR VNAA20260125017](https://openairdocs.org/sdr/VNAA20260125017.md): Bracket · cracked · Dec 13, 2025 · N601EN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACKED SLAT TRACK, 1-3 CANNISTER WELDED BRACKET AT THE LT WING FUEL TANK. THE CRACKED CANNISTER WELDED BRACKET AT THE LT WING FUEL TANK WAS REPAIR IAW REO 670-57-42-577 REV -.
- [SDR VNAA20260125016](https://openairdocs.org/sdr/VNAA20260125016.md): Handle · worn · Dec 12, 2025 · N601EN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR ON EXTERNAL SKIN OF EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. THE HANDLE AND HOUSING OF THE AFT CARGO DOOR WERE REPLACED IAW AMM 52-31-03-400-801,CONFIGA 1.
- [SDR VNAA20260125001](https://openairdocs.org/sdr/VNAA20260125001.md): Floor Support · cracked · Dec 12, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACKED COCKPIT FLOOR SUPPORT LBL 12 TO FLOORBEAM BS 280. THE FLOOR SUPPORT BELOW FLIGHT COMPARTMENT. THE CRACKED COCKPIT FLOOR SUPPORT WAS REPAIRED IAW REO 690-53-11-2102, REV --.
- [SDR VNAA20260125023](https://openairdocs.org/sdr/VNAA20260125023.md): Seat Track · corroded · Dec 11, 2025 · N601EN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE SIDE SEAT TRACK TWO SEGMENTS AT S15L, BS 785 TO BS 847 + 8.40. AND BS 847 + 35 - BS 902. EVALUATED, THE SEAT TRACKS WERE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, AND SRM 53-51-49-101-001-A02, AND REPLACED IAW AMM 53-00-49.
- [SDR VNAA20260125022](https://openairdocs.org/sdr/VNAA20260125022.md): Seat Track · corroded · Dec 11, 2025 · N601EN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES & SCRATCHES ON THE SIDE SEAT TRACK, S15R BTW BS 379 TO 720.85 AND SIDE SEAT TRACK, S15L BTW BS 379 TO BS 720.85. THE TWO SIDE SEAT TRACKS WERE EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-41-49-101-001-A02, AND REPLACED IAW AMM 53-00-
- [SDR VNAA20260125014](https://openairdocs.org/sdr/VNAA20260125014.md): Seat Track · corroded · Dec 11, 2025 · N601EN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT RAIL AT LBL 9 BS 374 TO 485. THE SEAT TRACK WAS EVALUATED OUT LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-21-49-101-001-A02, & REPLACED IAW AMM 53-00-49-400-801, CONFIG A12.
- [SDR VNAA20260125013](https://openairdocs.org/sdr/VNAA20260125013.md): Seat Track · corroded · Dec 11, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORRODED SEAT TRACK, 3 SEGMENTS AT RBL 9, BS 348 TO 360, BS 360 TO 485, AND BS 485 TO 581. THE SEAT TRACK SEGMENTS WERE EVALUATED OUT OF LIMITS IAW SRM 51-10-06-001-001-A01, & REPLACED IAW AMM 53-00-49-400-801, CONFIG A12.
- [SDR VNAA20260125012](https://openairdocs.org/sdr/VNAA20260125012.md): Seat Track · corroded · Dec 11, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON SIDE SEAT RAIL 02 SEGMENTS AT STGR15L, (01 SEG.) FS785.00 TO FS847.00 + 8.40. AND (02 SEG.) FS847.00 + 35.00 TO FS902. DUE TO EXCESS DAMAGE ALONG THE RAIL ON SIDE SEAT RAIL 02 SEGMENTS AT STGR15R, (01 SEG.) FS785.00 TO FS847.00 + 8.40. AND (02 SE
- [SDR VNAA20260125010](https://openairdocs.org/sdr/VNAA20260125010.md): Floorbeam · corroded · Dec 10, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM ANGLE BS 280, 9 LBL - 9 RBL IN THE COCKPIT. FLOORBEAM SUPPORT ANGLE BS 280 9 LBL - 9 RBL WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-13-001-001-A01.
- [SDR VNAA20260125008](https://openairdocs.org/sdr/VNAA20260125008.md): Cap · corroded · Dec 9, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON MIDCAP OF EXTERNAL SURROUND STRUCTURE OF PASSENGER DOOR. MIDCAP OF EXTERNAL SURROUND STRUCTURE OF PASSENGER DOOR WAS REPLACED IAW SRM 51-41-02-001-001-A01.
- [SDR VNAA20260125007](https://openairdocs.org/sdr/VNAA20260125007.md): Drag Angle · cracked · Dec 9, 2025 · N601EN · Bombdr CL6002D15 · Fuselage, Stabilizer Attach Fittings
  > CRACKED LEFT VERTICAL STAB TO AFT FUSELAGE ATTACHMENT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS RE
- [SDR VNAA20260125006](https://openairdocs.org/sdr/VNAA20260125006.md): Web · cracked · Dec 9, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BS 193, WL 79.50, S16R, INTERNAL FORWARD EQUIPMENT COMPARTMENT. THE WEB WAS REPAIRED IAW SRM 53-11-43-201-001-A01.
- [SDR VNAA20260125005](https://openairdocs.org/sdr/VNAA20260125005.md): Skin · worn · Dec 9, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL FUSELAGE SKIN, STRINGER 27 BTW BS 911 TO BS 919. EXTERNAL FUSELAGE SKIN WAS REPAIRED IAW REO 690-53-51-532 REV--.
- [SDR VNAA20260125003](https://openairdocs.org/sdr/VNAA20260125003.md): Skin · dented · Dec 9, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > DENT BS 954, STR 22L WITHIN 1515.79 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. DENT OF BS 954 BTW STR 22L-23L WAS REPAIRED PER REO 690-53-51-535 REV--.
- [SDR VNAA20260125004](https://openairdocs.org/sdr/VNAA20260125004.md): Landing · cracked · Dec 8, 2025 · N601EN · Bombdr CL6002D15 · Fuselage Main, Structure
  > ADG LANDING DOOR CRACK WITHIN 1438 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. UPPER DOOR LANDING WAS REPLACED IAW SRM 51-42-21-001-001-A01, AND SRM 51-42-06-001-001-A01.
- [SDR VNAA20260125002](https://openairdocs.org/sdr/VNAA20260125002.md): Skin · dented · Dec 8, 2025 · N601EN · Bombdr CL6002D15 · Wing, Plate/Skin
  > DENT DAMAGE TO INBD LOWER WING T/E SKIN BETWEEN WS 14.500 AND WS 50.000, THE WING TE SKIN BETWEEN WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 & AT FITTING ASSY WAS REPAIRED IAW EA 5750-2026-0060, REV--.
- [SDR VNAA20260125011](https://openairdocs.org/sdr/VNAA20260125011.md): Skin · dented · Dec 7, 2025 · N601EN · Bombdr CL6002D15 · Nacelle/Pylon, Plate/Skin
  > SEVERAL DENTS BTW THE 4 O'CLOCK TO 7 O'CLOCK ON THE LOWER EXTERNAL SKIN OF FAN COWL DOOR AND INLET COWL AT LT ENGINE. SKIN SKIN ON THE LEFT INLET COWL WAS REPAIRED IAW REO 690-54-11-592 REV - MUST BE ATTENDED ON NRC00267.
- [SDR VNAA2025082711102](https://openairdocs.org/sdr/VNAA2025082711102.md): Tire · blown · Aug 25, 2025 · N601EN · Cndair CL6002D24 · Tire
  > RTF-NO 2 MLG TIRE BLOWN ON TO. REMOVED AND REPLACED LIB MAIN TIRE IAW CRJ AMM 32-41-01-000-801-A01-PSA.
- [SDR VNAA2022113000004](https://openairdocs.org/sdr/VNAA2022113000004.md): Seat Track · corroded · Nov 8, 2022 · N601EN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK, RBL 9, BS 349 - 485 IN THE PASSENGER CABIN.
- [SDR VNAA2022113000003](https://openairdocs.org/sdr/VNAA2022113000003.md): Step · cracked · Nov 3, 2022 · N601EN · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON PASSENGER DOOR STEP PANEL 832DT
- [SDR VNAA2022113000002](https://openairdocs.org/sdr/VNAA2022113000002.md): Skin · corroded · Nov 3, 2022 · N601EN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN CUT OUT, SEAL SETTLEMENT AREA, DOOR SURROUND STRUCTURE, MAIN AVIONIC COMPARTMENT.
- [SDR VNAA2022113000001](https://openairdocs.org/sdr/VNAA2022113000001.md): Skin · damaged · Nov 3, 2022 · N601EN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > NICKS ON EXTERNAL FUSELAGE SKIN BTW STGR 27 AND 26LH, BTW FS 517.00 TO FS 565.00 AND BTW FS 629.00 TO FS 661.00 + 16.00
- [SDR VNAA202205231111](https://openairdocs.org/sdr/VNAA202205231111.md): Smoke Detector · unserviceable · May 20, 2022 · N601EN · Cndair CL6002D24 · Smoke Detection
  > CREW REPORTED REJECTED TAKEOFF AT MKE USING RUNWAY 25L AT AN APPROXIMATE SPEED OF 115KTS. CREW RECEIVED A WARNING MESSAGE FROM THE SMOKE DETECTOR IN THE FROM LAVATORY. MAINTENANCE IS CURRENTLY INSPECTING AIRCRAFT. DEFERRED PER MEL 26-16-01 CAT C, M/FC CW. EMPT
- [SDR VNAA202108201111](https://openairdocs.org/sdr/VNAA202108201111.md): A/C Pack · inoperative · Aug 17, 2021 · N601EN · Cndair CL6002D24 · Cabin Cooling System
  > DURING FLIGHT, AT FL360 THE RH PACK WENT INOP. AS OUR LIMITATION STATES 1 PACK OPERATION MUST BE FL310 OR BELOW, THE CREW REQUESTED THE DESCEND TO COMPLY. ATC COULD NOT PROVIDE THIS, SO THE CREW DECLARED. AFTER DESCENDING, AND CONTINUING ON, THE PACK RESUMED F
- [SDR VNAA2020031431101](https://openairdocs.org/sdr/VNAA2020031431101.md): Sensor · malfunctioned · Mar 13, 2020 · N601EN · Cndair CL6002D24 · Cabin Cooling System
  > LEFT PACK TEMP AMBER MSG OCCURRED DURING CLIMB. FLIGHT THEN RETURNED TO FIELD IN CLT. REMOVED AND REPLACED LEFT PACK COMPRESSOR DISCHARGE TEMP SENSOR IAW CRJ 900 AMM 21-51-10-000/400-801. OPS CHECK GOOD.
- [SDR VNAA201911121101](https://openairdocs.org/sdr/VNAA201911121101.md): Flashlight · inoperative · Nov 11, 2019 · N601EN · Cndair CL6002D24 · Emergency Equipment
  > AFT FLASHLIGHT INOP. - REMOVED AND REPLACED AFT FLASHLIGHT ASSEMBLY, OPS CHECK GOOD.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N601EN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N601EN/reports

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